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    Novel Extreme Learning Machine Using Kalman Filter for Performance Prediction of Aircraft Engine in Dynamic Behavior

    Source: Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 005
    Author:
    Feng Lu
    ,
    Jindong Wu
    ,
    Jinquan Huang
    ,
    Xiaojie Qiu
    ,
    Zhaoguang Wang
    DOI: 10.1061/(ASCE)AS.1943-5525.0001167
    Publisher: ASCE
    Abstract: In this paper, a novel state-propagation extreme learning machine using a Kalman filter (KF-ELM) is proposed. In comparison with the plain extreme learning machine, the proposed algorithm takes the topological parameters as state variables and minimizes the covariance of state estimates to overcome the state conjunction and transformation dilemma in time series. As a result, its topological stability and prediction accuracy are enhanced, and these merits are further proved theoretically. In addition, the computational effort of KF-ELM is on the same order of magnitude as the plain extreme learning machine, while the former possesses a faster convergent speed. Then, several benchmark datasets are utilized to test the effectiveness and soundness of the proposed algorithm. Finally, it is employed to predict the gas path performance of a turbofan engine. The performance prediction accuracy is better than the plain ELM with different input rules in the dynamic process. Particularly under various flight operation conditions, the proposed algorithm performs well and its stability is sufficiently showcased. In a word, the proposed algorithm provides a candidate technique for predicting aircraft engine performance in dynamic behavior.
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      Novel Extreme Learning Machine Using Kalman Filter for Performance Prediction of Aircraft Engine in Dynamic Behavior

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4268542
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    contributor authorFeng Lu
    contributor authorJindong Wu
    contributor authorJinquan Huang
    contributor authorXiaojie Qiu
    contributor authorZhaoguang Wang
    date accessioned2022-01-30T21:37:19Z
    date available2022-01-30T21:37:19Z
    date issued9/1/2020 12:00:00 AM
    identifier other%28ASCE%29AS.1943-5525.0001167.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4268542
    description abstractIn this paper, a novel state-propagation extreme learning machine using a Kalman filter (KF-ELM) is proposed. In comparison with the plain extreme learning machine, the proposed algorithm takes the topological parameters as state variables and minimizes the covariance of state estimates to overcome the state conjunction and transformation dilemma in time series. As a result, its topological stability and prediction accuracy are enhanced, and these merits are further proved theoretically. In addition, the computational effort of KF-ELM is on the same order of magnitude as the plain extreme learning machine, while the former possesses a faster convergent speed. Then, several benchmark datasets are utilized to test the effectiveness and soundness of the proposed algorithm. Finally, it is employed to predict the gas path performance of a turbofan engine. The performance prediction accuracy is better than the plain ELM with different input rules in the dynamic process. Particularly under various flight operation conditions, the proposed algorithm performs well and its stability is sufficiently showcased. In a word, the proposed algorithm provides a candidate technique for predicting aircraft engine performance in dynamic behavior.
    publisherASCE
    titleNovel Extreme Learning Machine Using Kalman Filter for Performance Prediction of Aircraft Engine in Dynamic Behavior
    typeJournal Paper
    journal volume33
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001167
    page14
    treeJournal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 005
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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